AD 90-05-11

final rule

Airworthiness Directives; British Aerospace Model BAe 146-100A and -200A series airplanes

AD Number
90-05-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
89-NM-233-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft BAE Systems (Operations) Limited BAe 146-100A Airworthiness Directives; British Aerospace Model BAe 146-100A and -200A series airplanes
aircraft BAE Systems (Operations) Limited BAe 146-200A Airworthiness Directives; British Aerospace Model BAe 146-100A and -200A series airplanes

Unsafe Condition

Inability of the flap system to sustain expected loads and reduction of airplane controllability.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Install new roller bearing pins at the forward top position on the right and left flap track No. 3 lower carriage assemblies in accordance with British Aerospace Service Bulletin 57-24-00911A, Revision 1, dated May 1, 1988. Alternate means of compliance or adjustment of compliance time may be approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

within 180 days after the effective date of this AD, unless previously accomplished

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

British Aerospace Model BAe 146-100A and -200A series airplanes as listed in British Aerospace Service Bulletin 57-24-00911A, Revision 1, dated May 1, 1988

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Flap Track

Applicability Source Text

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AD Number:
90-05-11
Document Type:
AD Final Rules
Docket Number:
89-NM-233-AD
Subject Heading:
Airworthiness Directives; British Aerospace Model BAe 146-100A and -200A series airplanes
Subject:
Flap Track
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/09/1990
Make:
BAE Systems (Operations) Limited
Model:
BAe 146-100A | BAe 146-200A
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 90-05-11
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-233-AD

AMENDMENT:   39-6525

AD NUMBER:   90-05-11

SUBJECT HEADING:   Airworthiness Directives; British Aerospace Model BAe 146-100A and -200A series airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 9, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-05-11 BRITISH AEROSPACE: Amendment 39-6525. Docket No. 89-NM-233-AD.
Applicability: Model BAe 146-100A and -200A series airplanes, as listed in British Aerospace Service Bulletin 57-24-00911A, Revision 1, dated May 1, 1988, certificated in any category.

Compliance: Required within 180 days after the effective date of this AD, unless previously accomplished.

To prevent inability of the flap system to sustain expected loads and prevent reduction of airplane controllability, accomplish the following:

A. Install new roller bearing pins at the forward top position on the right and left flap track No. 3 lower carriage assemblies, in accordance with British Aerospace Service Bulletin 57-24-00911A, Revision 1, dated May 1, 1988.

B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Standardization Branch, ANM-113.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to British Aerospace, Librarian for Service Bulletins, P.O. Box 17414, Dulles International Airport, Washington, D.C. 20041. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Standardization Branch, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6525, AD 90-05-11) becomes effective on April 9, 1990.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_90-05-11.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
90-05-11
Document Type:
AD Final Rules
Docket Number:
89-NM-233-AD
Subject Heading:
Airworthiness Directives; British Aerospace Model BAe 146-100A and -200A series airplanes
Subject:
Flap Track
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/09/1990
Make:
BAE Systems (Operations) Limited
Model:
BAe 146-100A | BAe 146-200A
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 90-05-11
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-233-AD

AMENDMENT:   39-6525

AD NUMBER:   90-05-11

SUBJECT HEADING:   Airworthiness Directives; British Aerospace Model BAe 146-100A and -200A series airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 9, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-05-11 BRITISH AEROSPACE: Amendment 39-6525. Docket No. 89-NM-233-AD.
Applicability: Model BAe 146-100A and -200A series airplanes, as listed in British Aerospace Service Bulletin 57-24-00911A, Revision 1, dated May 1, 1988, certificated in any category.

Compliance: Required within 180 days after the effective date of this AD, unless previously accomplished.

To prevent inability of the flap system to sustain expected loads and prevent reduction of airplane controllability, accomplish the following:

A. Install new roller bearing pins at the forward top position on the right and left flap track No. 3 lower carriage assemblies, in accordance with British Aerospace Service Bulletin 57-24-00911A, Revision 1, dated May 1, 1988.

B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Standardization Branch, ANM-113.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to British Aerospace, Librarian for Service Bulletins, P.O. Box 17414, Dulles International Airport, Washington, D.C. 20041. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Standardization Branch, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6525, AD 90-05-11) becomes effective on April 9, 1990.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.